What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23)On June 9, 2000, at apporximately 1341 EDT, a british aerospace jetstream 3201, N914AE, operated by cc air, dab U.S. Air express under the call sign "carolina 5224" made an emegency landing due to an apparent engine failure and engine fire. The airplane was operating in visual meteorological conditions (VMC) weather conditions on an IFR flight plan under 14 CFR 121 form charlotte, NC. The preliminary inspection of aircraft damage appears to be contained to the number 1 (left) engine which consisted of the following: accessary gearbox (case housing), gearbox drive gears (fractured/fragmented planet and sun gears), starter-generator (drive sheared), inlet stator vanes (deep gouges/gauling), and engine cowling (heat scoring from fire). The rated airline transport pilot/captain; his first officer, and (11) paasengers were not injuried. The captain stated the "we were beginning the descent form 11,000 feet when we heard a loud noise with a left yaw." "Subsequently, the fire warning system activated indicating an engine fire at the #1 engine." The crew executed the appropriate emergency procedures and secured the #1 engine with one fire bottle application. The captain also s tated that some smoke entered the cabin briefly, but dissipated immediately upon securing the failed engine. Reveiw of maintenance records did not reveal any previous abnormalities with either engine of airframe components. Weather conditions at the time of the incident was VFR, winds 210 degrees at 7 knots.
As the FAA filed it
(-23)ON JUNE 9, 2000, AT APPORXIMATELY 1341 EDT, A BRITISH AEROSPACE JETSTREAM 3201, N914AE, OPERATED BY CC AIR, DAB U.S. AIR EXPRESS UNDER THE CALL SIGN "CAROLINA 5224" MADE AN EMEGENCY LANDING DUE TO AN APPARENT ENGINE FAILURE AND ENGINE FIRE. THE AIRPLANE WAS OPERATING IN VISUAL METEOROLOGICAL CONDITIONS (VMC) WEATHER CONDITIONS ON AN IFR FLIGHT PLAN UNDER 14 CFR 121 FORM CHARLOTTE, NC. THE PRELIMINARY INSPECTION OF AIRCRAFT DAMAGE APPEARS TO BE CONTAINED TO THE NUMBER 1 (LEFT) ENGINE WHICH CONSISTED OF THE FOLLOWING: ACCESSARY GEARBOX (CASE HOUSING), GEARBOX DRIVE GEARS (FRACTURED/FRAGMENTED PLANET AND SUN GEARS), STARTER-GENERATOR (DRIVE SHEARED), INLET STATOR VANES (DEEP GOUGES/GAULING), AND ENGINE COWLING (HEAT SCORING FROM FIRE). THE RATED AIRLINE TRANSPORT PILOT/CAPTAIN; HIS FIRST OFFICER, AND (11) PAASENGERS WERE NOT INJURIED. THE CAPTAIN STATED THE "WE WERE BEGINNING THE DESCENT FORM 11,000 FEET WHEN WE HEARD A LOUD NOISE WITH A LEFT YAW." "SUBSEQUENTLY, THE FIRE WARNING SYSTEM ACTIVATED INDICATING AN ENGINE FIRE AT THE #1 ENGINE." THE CREW EXECUTED THE APPROPRIATE EMERGENCY PROCEDURES AND SECURED THE #1 ENGINE WITH ONE FIRE BOTTLE APPLICATION. THE CAPTAIN ALSO S TATED THAT SOME SMOKE ENTERED THE CABIN BRIEFLY, BUT DISSIPATED IMMEDIATELY UPON SECURING THE FAILED ENGINE. REVEIW OF MAINTENANCE RECORDS DID NOT REVEAL ANY PREVIOUS ABNORMALITIES WITH EITHER ENGINE OF AIRFRAME COMPONENTS. WEATHER CONDITIONS AT THE TIME OF THE INCIDENT WAS VFR, WINDS 210 DEGREES AT 7 KNOTS.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.
Other reports on N914AE · 2
Matched to the same aircraft by N-number and date.